/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  1.4.1                                 |
|   \\  /    A nd           | Web:      http://www.openfoam.org               |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/

FoamFile
{
    version 2.0;
    format ascii;

    root "/home/elisa/TESI/MESH_GENERATION/GAMBIT_JOU/RAEplane/460k";
    case "RAEplane460k";
    instance "constant";
    local "polyMesh";

    class polyBoundaryMesh;
    object boundary;
}

// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

10
(
wingL
{
    type patch;
    physicalType slip;
    nFaces 22716;
    startFace 881968;
}

wingR
{
    type patch;
    physicalType slip;
    nFaces 22634;
    startFace 904684;
}

tail
{
    type patch;
    physicalType slip;
    nFaces 41;
    startFace 927318;
}

fuselage
{
    type patch;
    physicalType slip;
    nFaces 27653;
    startFace 927359;
}

lateralL
{
    type patch;
    physicalType extrapolatedOutlet;
    nFaces 168;
    startFace 955012;
}

lateralR
{
    type patch;
    physicalType extrapolatedOutlet;
    nFaces 168;
    startFace 955180;
}

top
{
    type patch;
    physicalType extrapolatedOutlet;
    nFaces 166;
    startFace 955348;
}

outlet
{
    type patch;
    physicalType extrapolatedOutlet;
    nFaces 150;
    startFace 955514;
}

bottom
{
    type patch;
    physicalType extrapolatedOutlet;
    nFaces 166;
    startFace 955664;
}

inlet
{
    type patch;
    physicalType supersonicInlet;
    nFaces 150;
    startFace 955830;
}
)

// ************************************************************************* //
